Advanced Research Foundation · Russia

Cyclocar

Advanced Research Foundation Cyclocar

矢量推力 · 概念设计 · 核查 2026-10-01

下列为 VFS 目录披露的参数，包含设计目标及历史版本信息。目录阶段不等于适航或量产状态；不同任务条件的航程与载荷不能直接当作同一条件下的性能。

主要参数

座位／载员: 6 passengers
乘客: 未公开／未录入
驾驶方式: Autonomous
航程（按来源口径）: 500 km (311 miles)
巡航速度: 未公开／未录入
最大速度: 250 km/h (155 mph)
最大起飞重量: 未公开／未录入
载荷: 600 kg (1,323 lb)
空重: 未公开／未录入
长度: 未公开／未录入
翼展: 未公开／未录入
高度: 未公开／未录入
动力来源: Hybrid-electric power source
电机: Possibly 4 electric motors or more
旋翼／螺旋桨: 未公开／未录入
续航时间: 未公开／未录入
飞行高度: 未公开／未录入
安全设计: Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. Two of the cyclical propellers can stop working and the aircraft can continue to fly and land safely. The aircraft will also have a whole aircraft parachute system.

Aircraft type: Passenger or air cargo hybrid-electric VTOL aircraft (concept design)
Piloting: Autonomous
Capacity: 6 passengers
Maximum speed: 250 km/h (155 mph)
Range: 500 km (311 miles)
Maximum payload: 600 kg (1,323 lb)
Cyclical propellers: 4 cyclical propellers
Electric Motors: Possibly 4 electric motors or more
Power source: Hybrid-electric power source
Fuselage: Carbon fiber composite
Windows: Canopy over the passenger seating area
Landing gear: Fixed quadricycle wheeled landing gear
Safety Features: Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. Two of the cyclical propellers can stop working and the aircraft can continue to fly and land safely. The aircraft will also have a whole aircraft parachute system.